CN201897576U - X-ray flaw detection fixture for annular part of air engine - Google Patents
X-ray flaw detection fixture for annular part of air engine Download PDFInfo
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- CN201897576U CN201897576U CN 201020637944 CN201020637944U CN201897576U CN 201897576 U CN201897576 U CN 201897576U CN 201020637944 CN201020637944 CN 201020637944 CN 201020637944 U CN201020637944 U CN 201020637944U CN 201897576 U CN201897576 U CN 201897576U
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Abstract
The utility model belongs to the technology of X-ray flaw-detection film loading, which relates to an X-ray flaw detection fixture for an annular part of an air engine. The X-ray flaw detection fixture for the annular part of the air engine comprises two elastic clips and a junction plate (4), wherein the two elastic clips are made of metal sheets; the junction plate (4) is used for connecting the two elastic clips; and each elastic clip is formed by connecting an upper resilient trip (2), a vertical plate (1) and a lower resilient trip (3). The X-ray flaw detection fixture for the annular part of an air engine is convenient to operate, a film can be loaded by only one person, the film loading efficiency is greatly improved, and quality for loading films and detecting flaws is guaranteed.
Description
Technical field
The utility model belongs to x-ray detection load technology, relates to a kind of aeromotor ring-shaped work pieces x-ray detection anchor clamps.
Background technology
During aeromotor is made, the ring-shaped work pieces of many different structures, different size and disk-like accessory need carry out the x-ray detection inspection, x-ray detection need be arranged exograph and stereotype in checking below part, the method that present load generally adopts is: with a plurality of agrafes stereotype and egative film are fixed to by on the lower surface of flaw detection part.Its shortcoming is: need many people's operations, load efficient is low; Because the opening of agrafe can not be adjusted, and has chamfering or thicker part to be difficult to clamp to some, make that load is bad to cause the flaw detection poor quality, the waste egative film also prolongs the flaw detection cycle.
Summary of the invention
The purpose of this utility model is: propose a kind ofly to be convenient to operate, load efficient height, can guarantee the aeromotor ring-shaped work pieces x-ray detection anchor clamps of load and flaw detection quality.
The technical solution of the utility model is: aeromotor ring-shaped work pieces x-ray detection anchor clamps is characterized in that two elasticity folders that it is made by sheet metal are formed with the web joint that is connected two elasticity folders; Each elasticity folder is connected to form by last flexure strip, riser and following flexure strip, last flexure strip, riser are identical with the width of following flexure strip, the inward flange of last flexure strip length direction is connected with the coboundary of riser is vertical, the inward flange of following flexure strip length direction is connected with the lower limb of riser is vertical, the length of last flexure strip is less than the length of following flexure strip, and the height of riser is not less than the thickness sum of the thickness and the exograph of the thickness of ring-shaped work pieces, stereotype; Web joint is a lath, and the riser that the left end of web joint and left side elasticity are pressed from both sides processes or weld by integral body or riveted joint is connected to integral body, and the riser of the right-hand member of web joint and right side elasticity folder is processed or welded or rivet by integral body and is connected to integral body.
The utility model has the advantages that: be convenient to operation, people is load easily just, has improved load efficient greatly, has guaranteed load and the quality of detecting a flaw.
Description of drawings
Fig. 1 is a structural representation of the present utility model.The part of being detected a flaw is represented in double dot dash line among the figure, and dotted line is represented stereotype and exograph.
Embodiment
Below the utility model is described in further details.Referring to Fig. 1, aeromotor ring-shaped work pieces x-ray detection anchor clamps is characterized in that, two elasticity folders that it is made by sheet metal are formed with the web joint 4 that is connected two elasticity folders; Each elasticity folder is connected to form by last flexure strip 2, riser 1 and following flexure strip 3, last flexure strip 2, riser 1 are identical with the width of following flexure strip 3, the vertical connection of coboundary of the inward flange of last flexure strip 2 length directions and riser 1, the vertical connection of lower limb of the inward flange of following flexure strip 3 length directions and riser 1, the length of last flexure strip 2 is less than the length of following flexure strip 3, and the height of riser 1 is not less than the thickness sum of the thickness and the exograph 6 of the thickness of ring-shaped work pieces, stereotype 5; Web joint 4 is laths, the riser 1 that the left end of web joint 4 and left side elasticity are pressed from both sides processes or weld by integral body or riveted joint is connected to integral body, and the riser 1 of the right-hand member of web joint 4 and right side elasticity folder is processed or welded or rivet by integral body and is connected to integral body.
Said flaw detection anchor clamps are processed into by the Thin Stainless Steel slab integral, the thickness δ=0.8mm～1.2mm of stainless sheet steel.
Using method of the present utility model is: during the dress exograph, earlier stereotype 5 and exograph 6 are positioned on the following flexure strip 3 of flaw detection anchor clamps, the flaw detection anchor clamps that will install stereotype 5 and exograph 6 then are installed to by on the flaw detection part 7, stereotype 5 and exograph 6 are positioned at by the lower surface of flaw detection part 7, and last flexure strip 2 is positioned at by the upper surface of flaw detection part 7.The utility model can be made different series of products, so that be suitable for different quilt flaw detection parts.
Thickness by flaw detection part 7 is 10mm, and the thickness of stereotype and exograph 6 is 10mm, and said flaw detection anchor clamps are processed into by the Thin Stainless Steel slab integral, and the thickness δ=1mm of stainless sheet steel, the height of riser 1 are 20mm.
Thickness by flaw detection part 7 is 15mm, and the thickness of stereotype and exograph 6 is 10mm, and said flaw detection anchor clamps are processed into by the Thin Stainless Steel slab integral, and the thickness δ=1.2mm of stainless sheet steel, the height of riser 1 are 25mm.
Thickness by flaw detection part 7 is 8mm, and the thickness of stereotype and exograph 6 is 10mm, and said flaw detection anchor clamps are processed into by the Thin Stainless Steel slab integral, and the thickness δ=0.8mm of stainless sheet steel, the height of riser 1 are 18mm.
Claims (2)
1. aeromotor ring-shaped work pieces x-ray detection anchor clamps is characterized in that, two elasticity folders that it is made by sheet metal are formed with the web joint [4] that is connected two elasticity folders; Each elasticity folder is connected to form by last flexure strip [2], riser [1] and following flexure strip [3], last flexure strip [2], riser [1] are identical with the width of following flexure strip [3], the inward flange of last flexure strip [2] length direction and vertical connection of coboundary of riser [1], the inward flange of following flexure strip [3] length direction and vertical connection of lower limb of riser [1], the length of last flexure strip [2] is less than the length of following flexure strip [3], and the height of riser [1] is not less than the thickness sum of the thickness and the exograph [6] of the thickness of ring-shaped work pieces, stereotype [5]; Web joint [4] is a lath, the riser [1] that the left end of web joint [4] and left side elasticity are pressed from both sides processes or weld by integral body or riveted joint is connected to integral body, and the riser [1] of the right-hand member of web joint [4] and right side elasticity folder is processed or welded or rivet by integral body and is connected to integral body.
2. aeromotor ring-shaped work pieces x-ray detection anchor clamps according to claim 1 is characterized in that it is processed into by the Thin Stainless Steel slab integral, the thickness δ=0.8mm～1.2mm of stainless sheet steel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201020637944 CN201897576U (en) | 2010-12-02 | 2010-12-02 | X-ray flaw detection fixture for annular part of air engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201020637944 CN201897576U (en) | 2010-12-02 | 2010-12-02 | X-ray flaw detection fixture for annular part of air engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201897576U true CN201897576U (en) | 2011-07-13 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201020637944 Expired - Fee Related CN201897576U (en) | 2010-12-02 | 2010-12-02 | X-ray flaw detection fixture for annular part of air engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201897576U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108168475A (en) * | 2017-12-18 | 2018-06-15 | 中国航发贵州黎阳航空动力有限公司 | The measuring method of transporter burner inner liner shaped air film hole Special angle |
| CN108534720A (en) * | 2018-06-26 | 2018-09-14 | 同济大学 | A kind of fixing device of the ultra-thin cylinder eyeglass of laser scanning test deep camber |
| CN110842798A (en) * | 2019-11-13 | 2020-02-28 | 陈明会 | Open precision positioning tool structure for machining arc edge of aviation precision casting part |
-
2010
- 2010-12-02 CN CN 201020637944 patent/CN201897576U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108168475A (en) * | 2017-12-18 | 2018-06-15 | 中国航发贵州黎阳航空动力有限公司 | The measuring method of transporter burner inner liner shaped air film hole Special angle |
| CN108534720A (en) * | 2018-06-26 | 2018-09-14 | 同济大学 | A kind of fixing device of the ultra-thin cylinder eyeglass of laser scanning test deep camber |
| CN110842798A (en) * | 2019-11-13 | 2020-02-28 | 陈明会 | Open precision positioning tool structure for machining arc edge of aviation precision casting part |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20110713 Termination date: 20151202 |
|
| EXPY | Termination of patent right or utility model |